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Landing Integrated Simulation for Reusable Launch Vehicle and Probe

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EDG20166 Subject Category: Research and Development PDF Responsible Representative: Taro Shimizu, Research and Development Directorate, Research Unit III Contact Information: Hiroaki Amakawa , Research Unit III, Research and Development Directorate. Japan Aerospace Exploration Agency(amakawa.hiroaki@jaxa.jp) Members: Hiroaki Amakawa, Masaru Kusano, Kaname Kawatsu, Kugo Okada Abstract In reusable rockets and probe landers, landing is a crucial part of the mission, and the success of the landing determines whether the mission is achieved.・・・<<read more>>

Thermal and Fluid Dynamics of the Atmospheric Reentry Capsule

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EDU10300 Subject Category: Space and Astronautical Science PDF Responsible Representative: Hideto Takasawa, ISAS, Dept. of Space Flight Systems Contact Information: Takasawa hideto(takasawa.hideto@jaxa.jp) Members: Shotaro Baba, Reo Iida, Tomohito Morimoto, Takahiro Miki, Hideto Takasawa Abstract During atmospheric entry, a capsule travels over a wide range of velocities from hypersonic to subsonic regimes. Consequently, this leads to severe aerodynamic heating and disturbances in its flight attitude. To elucidate and mitigate these phenomena,・・・<<read more>>

Research on Fundamental Aerodynamics in Real-World Environments

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EDA201J99 Subject Category: Aeronautical Technology PDF Responsible Representative: Nakita Kazuyuki, Aviation Technology Directorate, Fundamental Aeronautics Research Unit Contact Information: Yuki Ide, Chanteux Xavier(ide.yuki@jaxa.jp, chanteux.xavier@jaxa.jp) Members: Xavier Chanteux, Lusher David, Tokugawa Naoko, Ohhira Keisuke, Ide Yuki Abstract The project aims to improve understanding of the boundary-layer laminar-to-turbulent transition process in low-turbulence environment such as wind tunnel or flight conditions. One of the items of this project investigates the influence of free-stream・・・<<read more>>

Development of Defensive Technology for Particle Ingestion

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EDA201D10 Subject Category: Aeronautical Technology PDF Responsible Representative: Takeshi Fujiwara, Aviation Technology Directorate, Aviation Safety Innovation Hub Contact Information: Masaya Suzuki, Aviation Technology Directorate, Aviation Safety Innovation Hub(suzuki.masaya@jaxa.jp) Members: Kazuhisa Amemiya, Kazuto Fukui, Junichi Kazawa, Joe Matsutani, Naruto Mita, Rintaro Nakajima, Yota Nakamura, Jukito Oka, Yuya Ohashi, Masaya Suzuki, Kenji Shimizu, Mutsuki Sugiyama, Sota Tamehiro, Mizuki Watanabe Abstract The atmosphere in which aircraft fly is not ideal, with various fine・・・<<read more>>

Research on the rotorcraft aerodynamics and noise prediction technologies

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JAXA Supercomputer System Annual Report February 2025-January 2026 Report Number: R25EDA201G28 Subject Category: Aeronautical Technology PDF Responsible Representative: YASUE Kanako, Aviation Technology Directorate, Aviation Integration Innovation Hub Contact Information: IKEDA Tomoaki(ikeda.tomoaki@jaxa.jp) Members: Hirokazu Higashida, Manabu Hisida, Kenji Hayashi, Tomoaki Ikeda, Masatoshi Kanayama, Yuki Kishi, Hideji Saiki, Kanako Yasue Abstract We aim at the development of aerodynamics and noise computation techniques for rotorcrafts by the unstructured-grid CFD code FaSTAR-Move that utilizes an overset moving grid approach. Extracting the unsteady CFD data・・・<<read more>>